Commonwealth legislation

AD/ROBIN/16 - Ball and Socket Fitting

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

Requires inspection and any corrective action on ball‑and‑socket fittings of Robin ATL and R3000 aircraft, carried out per the manufacturer service bulletins (ROBIN SA SB No.8 Rev.1 for ATL; Avions Pierre Robin SB No.121 Rev.1 for R3000) before the next flight after 30 June 1992. Owners/operators must arrange and pay for compliance. Purpose: prevent jamming from a manufacturing surface‑treatment defect; action aligns with the related French DGAC AD.

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AD/ROBIN/16 - Ball and Socket Fitting

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Robin Aviation Series Aeroplanes

AD/ROBIN/16 Ball and Socket Fitting 7/92

Applicability: ATL, all types, and R3000, all types.

Requirement: For ATL: Action in accordance with ROBIN SA SB No.8 Rev.1.

For R3000: Action in accordance with AVIONS PIERRE ROBIN SB No.121 Rev.1.

Note: DGAC AD 91-154(A) refers.

Compliance: Unless already accomplished; Prior to further flight after 30 June 1992.

Background: The DGAC requires an inspection of the ball and socket fittings. This action is required in order to prevent jamming of certain ball and socket fittings, due to a surface treatment problem during manufacture.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.